Files
thesis/archive/ES_0.6323660859645353
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.6323660859645353---------------------------
Spacecraft: mySat
dry_mass: 200.0 kg
specific impulse: 3200.0 kg/s
max_thrust: 0.00025 kN
num_thrusters: 1
duty_cycle: 1.0
Launch Mass: 3500.0 kg
Launch Date: 2023-04-23T06:06:55.672
Launch V∞: [5.428777295635992, -8.63433740885306, -2.0354044213827263] km/s
Phase 1:
Planet: Saturn
V∞_in: [4.915840459079783e-5, 9.838133448777907e-6, -9.763921129437645e-6] km/s
V∞_out: [-3.162207398223452e-5, -3.2740195018376924e-5, -2.3537583349863486e-5] km/s
time of flight: 1.0622899927425869e8 seconds
arrival date: 2026-09-03T18:10:14.672
thrust profile: [0.8333743399556065 -0.6252515848665894 -0.4656654053990616; 0.33234581463537316 -0.0734223779319033 -0.33144542259183196; 0.13823751877850682 -0.0011233900839936767 -0.2032659715376126; 0.13030760726326296 0.014244570510876587 -0.23702860717166258; 0.04872796083201726 0.008897608606901811 -0.10736697911910557; 0.03149799643287016 0.0071139755872436415 -0.07714260912053336; 0.0253960149841122 0.007115334808249497 -0.06949854271963204; 0.01982226642326839 0.006085134735392963 -0.05853371527318575; 0.0013554625466232764 -0.0003586865833393831 0.0006247764592780558; -0.0009609707715594207 -0.0003615652488133268 -0.001614196172902163; 0.0004053797699357226 -0.00040216526947146707 -0.0007899195170559506; 0.000802833023965012 0.0009364772543747914 -0.002620512794072368; 0.0022044095705418282 -0.0027002328211821643 -0.0033624007458160597; 0.0002630394422776282 0.0011434200066028463 -0.002786278515575517; -0.0014182012152468473 -0.0003010747552525555 -0.010939547988884964; 0.0013491874406124996 0.0009348481207715033 -0.0020233582449547755; -0.000622626612388189 0.00102348348942637 -0.0017638091698732442; -0.0027122341774007365 -0.0037589614770834412 -0.008510212883989395; -0.0015202843915566905 -0.004177597829823361 0.0036063384634263057; 0.005544899855727037 -0.0030781489525088628 -0.0029958913038565663] %
Mass Used: 106.79048694294443 kg
Launch C3: 108.16627657411657 km²/s²
||V∞_in||: 5.1075158027072366e-5 km/s